Limitations Flashcards

0
Q

What is the normal operating pressure range of the hydraulic system?

A

3000 +/- 200psi

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1
Q

You have accepted 2 jumpseat passengers, but notice that the crew oxygen pressure display on the DOOR/OXY ECAM page shows a half Amber boxed pressure of 900psi

A

Dispatch is allowed, as long as the Ref Temeratur is less than 17°C

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2
Q

The maximum altitude with 2 Packs and Elec supplied by the APU is?

A

17500ft

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3
Q

IN-SEAT POWER SUPPLY SYSTEM (ISPSS)

A

Must be switched off for takeoff and landing

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4
Q

Wind speed on the ground during a turn-around is currently 35kt but forecast to increase to 60kt

A

Th pax doors and the cargo doors may be operated. However, the cargo doors cannot be operated above 40kt (50kt with the aircraft nose into the wind, or with the cargo door on the leeward side)

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5
Q

The maximum wind for cargo door operation is:

A

40kt, or 50kt if aircraft nose is oriented into the wind

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6
Q

For a CAT3 approach ATHR:

A

Must be used in selected or managed speed

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7
Q

The engine is capable of starting

A

In crosswinds up to 35kts

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8
Q

What is the minimum engine oil quantity allowed for dispatch

A

Not less than 11 quarts plus 0.3 quarts per hour of flight time (maximum)

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9
Q

The turbulence speed for B-HTE is?

A

270kt up to FL200 then 300kt / M0.76 in an A321

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9
Q

In B-HTD fuel is fed to the wing tanks

A

Automatically via jet pumps, when the transfer logic is satisfied

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9
Q

For the A321 the speed brake extension is inhibited when

A

The flaps are in config 3 or Full

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9
Q

A FAULT light in the MODE SEL pb-sw on theA321 overhead fuel panel indicates

A

The center tank has more than 250kg of fuel and the left or right wing tank has less than 5000kg and the MODE SEL pb-sw is at auto

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9
Q

Under normal circumstances refuelling will take approximately?

A

In the A320 aircraft 17 minutes for the wings / 20 min for all tanks

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10
Q

Maximum ramp weight for A321 is

A

89.4T

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11
Q

The maximum wind condition for CAT III automatic approach or automatic landing and automatic rollout are

A

Headwind 30kt, Tailwind 10kt, Crosswind 20kt in an A321

12
Q

Comparing Maximum reverse thrust use in the A320 and A321

A

Should not be used above 70kts airspeed when the indication starts to fluctuate A320

13
Q

During a go-around due to windshear on APP HKG 07L the IAS reduces below 165kts after the flap lever is moved to zero

A

Slat retraction occurs normally A321